Researchers at Langley started an effort
to explore engine cowlings under the direction of Fred Weick, a young
Chicago-born engineer. Weick designed ten different cowlings, from a
partial covering to a complete covering of the engine. These were fitted
to a Wright Apache biplane with a J-5 Whirlwind air-cooled engine. The
goal was to produce a cowling that reduced drag but still cooled the
engine as much as an uncovered engine.
The ten cowlings were tested on the
engine in Langley's PRT. Engineers measured drag, propulsive efficiency of
the propeller (in other words, how efficient was the propeller at pushing
air past the cowlings), and the engine temperature. The best versions of
the cowlings were then modified, with the addition of vents and with
changes in their shape. This was all done in a methodical manner.
Eventually, the engineers decided upon a cowling design they designated
"No. 10," which completely covered the engine and its protruding cylinder
heads, letting in air at the front. The air was then directed over the
hottest parts of the engine and out the sides along the fuselage. What
they also learned was that the shape of the airplane behind the cowling
was important to understanding how to design the cowling in the first
place—the cowling had to smoothly connect to the fuselage so that the air
flowing over it was not disrupted.
The No. 10 cowling reduced drag by a
factor of almost three. This was such an impressive improvement in
performance that Weick chose to make the results public immediately so
that industry could take advantage of them. In November 1928, Weick wrote
Technical Note 301, directed at airplane manufacturers, which described
the cowling. Weick stated that using a cowling that completely covered the
engine was practical, but warned that "it must be carefully designed to
cool properly." The NACA's Washington office announced that a cowling
could be installed for about $25 per airplane and that the possible
overall savings from the industry's use of the cowling was at least $5
million (which was more than had been spent on the NACA since its
establishment in 1915).
Langley engineers then mounted cowling
No. 10 onto a borrowed Curtiss Hawk AT-5A biplane that used the same
Wright Whirlwind J-5 engine that had been tested in the PRT. The tests
showed that the airplane's maximum speed increased from 118 to 137 miles
per hour (190 to 220 kilometres per hour) with the cowling. On February
4-5, 1929, Frank Hawks, a barnstorming pilot, flew a Lockheed Air Express
equipped with a NACA low-drag cowling from Los Angeles to New York
non-stop
and established a new record. Hawks flew this distance in 18 hours and 13
minutes in an airplane whose top speed had been increased from 157 to 177
miles per hour (253 to 285 kilometres per hour). Gerry Vultee, of
Lockheed, sent the NACA a telegram that stated, "Cooling carefully checked
and OK. Record impossible without new cowling. All credit due NACA for
painstaking and accurate research." Soon many new speed records were being
established with aircraft equipped with versions of the NACA low-drag
cowling. In January 1930, the National Aeronautic Association awarded the
NACA the Collier Trophy for the greatest achievement in American aviation
in 1929.
The engine cowling was an important
technological development. But its importance was not so much developing a
thing as it was improving understanding of aeronautical design
techniques. Airplane designers could not simply stick an "engine
cowling"—a piece of tin—on any aircraft and have it work. They had to
specially design a cowling for each aircraft. But once they understood the
principles behind this device, and once they understood the method for
developing it, they could design engine cowlings for existing and new
aircraft and improve their efficiency. This then led to further research
on the proper placement and cooling of propeller engines, particularly on
large multi-engine craft, such as bombers. For instance, most multi-engine
craft before the mid-1930s, such as the Ford Trimotor, had the engines
mounted below the wings in pods (or "nacelles"). But further research at
the NACA, using the same methods developed for the low-drag cowling
development, demonstrated that the best place to mount the engines was
directly in front of the wing, blended into it. Thereafter, planes like
the B-17 bomber had engines that were fitted into the wing itself and
achieved greater efficiency.